US1952953A - Fatigue testing machine - Google Patents

Fatigue testing machine Download PDF

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US1952953A
US1952953A US530495A US53049531A US1952953A US 1952953 A US1952953 A US 1952953A US 530495 A US530495 A US 530495A US 53049531 A US53049531 A US 53049531A US 1952953 A US1952953 A US 1952953A
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cable
wheel
sleeve
testing
testing machine
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US530495A
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Richard L Templin
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Howmet Aerospace Inc
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Aluminum Company of America
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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N3/00Investigating strength properties of solid materials by application of mechanical stress
    • G01N3/32Investigating strength properties of solid materials by application of mechanical stress by applying repeated or pulsating forces
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N2291/00Indexing codes associated with group G01N29/00
    • G01N2291/02Indexing codes associated with the analysed material
    • G01N2291/028Material parameters
    • G01N2291/02827Elastic parameters, strength or force

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  • This invention relates generally to the art of testing materials, and particularly to the testing of wires or cables to' determine their resistance to stresses set up by periodic forces.
  • the cables are subjected, in addition to the tensile stresses set up in them ln supporting their own weight, to periodic stresses that result from vibrations. These undesirable vibrations are ordinarily set up by the wind or other forces causing the cable to oscillate in the direction transverse to its length. p It will be readily appreciated that it is diilicult to obtain data regarding the vibrations of cables when they are mounted in their operating positions for the reason that it is inconvenient to make the necessary measurements, and the oscillations cannot be controlled to provide data over a com- 20 plete range of conditions.
  • An ⁇ object of my invention is to provide apparatus for testing cables to determine their resistance to fatigue as the result of repeated stresses.
  • a further object is to provide a cable- .25 testing apparatus capable of duplicating the conditionsl to which a cable is subjected when supported in a span of a transmission line'.
  • I provide supporting structures to which the ends of a cable to be testedare attached.
  • the supporting structures are mounted, for instance on the floor of a building, in such manner that vibrations will not be transmitted from one structure to the other through the oor of-v the building, and suitable means are provided for applying predetermined tensile force to the cable.
  • Suitable apparatus is provided, preferably mounted on one of the supporting structures, for causing the cable to vibrate in a. direction transverse to its length. This apparatus is mounted intermediate the ends of the cable to cause vibration in a longitudinal plane, and is adjustable to apply a predetermined force at predetermined frequency.
  • Fig. l is a more or less diagrammatic view in elevation of the cable-testing apparatus
  • Fig. 2 is a view in longitudinal section taken on the plane represented by the line II-H in Fig. 3, of the mechanism for causing the cable tor vibrate:
  • Fig. 3 is a view, partlyA cable-vibrating mechanism taken on the plane represented by the line III-III of Fig. 2;
  • Fig. 4 is a plan view, partly in horizontal section, of the cable-vibrating mechanism and its associated operating mechanism;
  • Fig. 5 is a view in cross section of the operating mechanism taken on the plane represented by the line V-V in Fig. 4.
  • the apparatus comprises two piers 1 and 2 for supporting, at its respective ends, a piece of wire or cable 3 to be tested.
  • 'I'he supporting piers 1 and 2 are preferably massive bodies of concrete or of other. suitable material, supported on the oor 4 of a building by means of seals or pads 5 of non-resonant material, as for instance sand, to prevent extraneous vibrations from being transmitted from the oor 4 to the cable 3 by way of the piers, hence preventing transmission of vibrations through the floor from one end of the cable to the other.
  • the piers may be spaced as desired to provide for receiving a piece of cable of suitable 4length for testing.
  • one end of cable 3 is rigidly secured to the pier 1 by means of any suitable anchor or cable clamp 6 attached at the rear edge of the pier 1 and elevated somewhat above its upper surface by means of a supporting structure 7 that may be made of I-beams or other structural elements.
  • a supporting structure 7 that may be made of I-beams or other structural elements.
  • the other end of the cable is supported on pier 2 by means of an anchor 8 connected to one arm of a bell crank 9, pivoted on a bracket 1l at the back of the pier, on the other arm of which is suspended a weight 12.
  • the eect of the weight 12 in applying tension to the cable may be changed .by adding to or taking from it disks 13, as is ordinarily done in adjusting the weights on a scale, or by providing any other convenient means for applying objects of known weight.
  • vibrations in a suspended cable may be caused by the wind, snow or ice loads, or by other forces'to which the transmission line may be subjected.
  • vibrations set up stresses within the material of the cable of a repeating nature that add to the initial tensile stress in the cable, and periodically raise the total stress to dangerously high values.
  • the vibrating mechanism' 20 is designed to apply to the cable 3 transverse vibrations in one longitudinal plane o f the cable, of predetermined amplitude and frequency.
  • This apparatus comprises essentially a ily wheel 21, jour-,
  • the fly wheel 21 is provided withan eccentrically mounted weight-22 which may be adjusted, relative to the center of rotation, to regulate the applied force and amplitude of vibration of the cable. To adjust the frequency of vibration, it is simply necessary to regulate the speed of rotation of the fly wheel.
  • the y wheel 21 is journalled for rotation by means of suitable ballbearings 23 on a substantially cylindrical sleeve or spindle that surroundsand is secured to the test cable 3.
  • the ends of the sleeve 24 are disposed between pairs of vertical guides or standards 25 that constitute part of a frame 26 for the vibrating mechanism.
  • the vertical guides 25V constrain the sleeveV 24, and consequently the cable 3, to motion in the vertical longitudinal plane of the cable. ⁇
  • the sleeve is provided e -are in turn threaded on the exterior of the spindle 24.
  • sleeves 31 may be unscrewed from the ends of the spindle, whereupon they engage the shoulders 30 and force the collets 28 out of conical bores 27.
  • the sleeve 24 is providedwith encircling ball-.bearings 32 held in p1aceonl the sleeve by lock nuts 33, the outer races of said ball-bearings fitting between the guide plates or bearings 34 mounted on the guides V25 provided on the frame 26.
  • the tops of the guides 25 in each pair are connected by a tie bar 35, near the middle of each of which there is an oil cup 36 from which oil is permitted to drip on the ball-bearings 32 to lubricate them and the guide plates 34. Such excess oil as may drip from the bearings is collected in the base of the frame 26.
  • a ⁇ suitable chamber 37 is provided within the y wheel 21 for receiving lubricant, such as grease, for lubricating the ball-bearings .23 that support the fly wheel on the spindle 24.
  • the eccentric weight 22 is in the shape of an annulus that encircles the hub of the fly wheel 21 and lies within a chamber 38 in one side of the wheel between the hub and the rim thereof.
  • the eccentric loading ring 22 is supported in the chamber 38 by means of two set screws 39 which pass through diametrically opposed openings in the rim of the wheel 21 and are threaded in similarly aligned openings through the ring 22 in such manner that the screws 39 lie on a. diameter' of the wheel 21.
  • the inner ends of the screws 39 contact with the hub of the wheel 21, and, in order to adjust the position o! the eccentric ring 22, it is merely necessary to loosen one of the screws and tighten the other screw to move the ring in the desired direction.
  • the inner ends of the screws are made conical and bear at one side upon a4 conical surface 40 on the hub of the wheel 21 in such manner that when the screws are tightened they will tend to force the ring 22 sidewise into frictional engagement with the web of-the y wheel 21. In this manner the ring 22 will be prevented from moving relative to the fly wheel 21 while the vibrating mechanism is inv operation.
  • the ring 22 is made with one side thicker than the other, as shown in Fig. 3, and so proportioned that when the thick or heavy side of the ring is adjacent to the hub of the wheel 21, as shown, the wheel 21 will be substantially in true running balance. As the ring 22 is moved from this position to its other extreme position, the degree of unbalance of the wheel is varied from zero to a maximum value. Hence by adjusting the position of the ring any desired degree of periodic force may be applied to the cable 3 within the limits of the apparatus.
  • the vibrating mechanism 20 is mounted on the pier 1 in such manner that it may be moved longitudinally thereof to position it relative to the xed end of the cable.
  • the frame 26 of the vibrating mechanism is secured to a base plate 41 that is in turn fastened on the upper surface of the pier 1 by anchor bolts 42.
  • a plurality of bolts 42 are provided so spaced that the base plate 41 may be disposed in either one oi. ⁇ two positions on the pier at different distances from the end of the cable. This is accomplished by using three equally spaced pairs, or a total of six anchor bolts, and positioning the base plate to engage one pair of bolts. at each of its ends.
  • the base plate 41 may engage, at the appropriate end, one of the other end pair of bolts and at its other end, the
  • the base plate 41 is provided with T-slots 43 extending longitudinally thereof and parallel to the cable 3.
  • the vibrating mechanism is mounted on the base plate 41 in such manner that it may be adjusted longitudinally to any position within the limits of the base plate. After being positioned it may be securely clamped in place by means of nuts 45 threaded on the Yupper ends of the bolts 44.
  • the transmission mechanism comprises a suitable electric motor 51 con'- nected to drive the vibrating mechanism by means of a suitable speed changing device 52 that turns a cone pulley 53 from one Aface of which a belt 54 extends, in substantially horizontal direction, to a belt pulley 55 on the hub of the y wheel 21.
  • variable speed mechanism 52 and the driving motor 51 are both mounted on a common bed plate 57 that is secured to a pair of longitudinal members 58 extending between the transverse members 48 of the frame 47.
  • the entire bed plate 57, together with the motor 51 and the transmission mechanism 52, may be moved along the long'tudinal members 58 of the frame 47 to bring any one of the three faces of the cone pulley 53 into alignment with the belt pulley 55 on the fly wheel of the vibrating mechanism.
  • the belt may be tightened by moving the entire driving mechanism'and its bed plate 57 in the direction away from the vibrating mechanism.
  • This is accomvplished by means of a well known adjusting screw 61 that is journalled in the bed plate 57 and has screw threaded engagement with an adjusting block 62 carried by a clamping plate 63 tted between the longitudinal members 58.
  • the adjusting block 62 is disposed adjacent one of the longitudinal members 58, and there is provided adjacent the other longitudinal member a similarly shaped clamp'ng block 64.
  • the blocks 62 and 64 are each provided with downwardly extending threaded shanks passing through the clamping plate 63 Aand provided at their lower ends with clamping nuts 65.
  • the variable speed-transmission mechanism 52 is of the friction type, comprising a frame 71 in which a shaft 72 is journalled on antiefriction bearings 73 at right angles to the shaft of the motor 51.
  • the cone pulley 53 is mounted on one end of the shaft, and at the other end is mounted a friction wheel 74 driven in a well known manner by a friction disk 75 carried on the shaft of the driving motor 51.
  • the motor shaft is provided, at its other end, with an adjustable thrustV bearing mechanism 76.
  • This adjustment is accomplished by moving the motor 51 in guideways 78 on the base plate 57 in such manner that it may be moved parallel to the shaft 72 on which the friction wheel 74 is mounted.'
  • the motor may be adjusted to the de'sn'ed position along the guideways 78 by means of a screw-thread adjusting mechanism 79 that may be operated by means of a hexagonal fitting 80 at the end of the shaft.
  • a sample of the cable to be tested is passed through the sleeve 24 of the vibrating mechanism 20 and suspended between the piers 1 and 2 in the manner described.
  • Initial tension is applied to the cable 3 by attaching the required amount of weights 13 to the bell-crank 9, and theA eccentric weight 22 is adjusted to exert the desired amount of force to vibrate the cable.
  • the frequency at which the force is to be applied is thenregulated by adjust-1, ⁇ ing the variable speed mechanism 52.
  • the appa-v ratus may then be operated until the cable 3 breaks from fatigue failure, or if the cable does not fail, the test may be continued for a predetermined number of reversals of stress in the cable.
  • the total number of reversals of stress imposed upon the cable 3 during a test may be recorded by means of a revolution counter 81 mounted on the transmission mechanism 52 and actuated by the shaft 72.
  • a cable testing apparatus comprising spaced supporting structures for supporting at its ends a cable to be tested, said supporting structures including non-resonant bases to isolate the same from each other and their surroundings, means for applying a tensional force to said cable, and means for imparting vibrations to the cable in a direction transverse to its length, said vibration-imparting means comprising an eccentrically-loaded iiy wheel mounted for rotation upon and positioned intermediate the ends of said cable.
  • a cable testing apparatus comprising a pair vof isolated supports, means for suspending a cable lmounted for longitudinal movement with respect to the ends of said cable.
  • a cable testing apparatus comprising spaced supporting structures for supporting at itsends a cable to be tested, a sleeve mounted on said cable in spaced relation to one end thereof, vertical guides disposed at each side of said sleeve, a fly wheel having an adjustable eccentric weight rotatably mounted on said sleeve and means for rotating theeccentrically-weighted -fly wheel whereby the cableis vibrated in a vertical longitudinal plane.
  • a cable-vibrating device adapted to be positioned intermediate the ends of a suspended cable, said device comprising a sleeve secured to said cable, a fly wheel rotatably mounted on said sleeve, and means for driving said ily wheel, said driving means comprising a motor-driven adjustable speed transmission whereby the frequency of vibration may be varied.
  • a cable testing apparatus comprising means for suspending a cable to be tested, vsaid means comprising massive supporting piers arranged in spaced relationship upon non-resonant bases, a cable clamp mounted on one of said piers, a bell crank pivotally mounted on said other pier, said cable having one end' attached to the cable clamp and its opposite end attached to one arm of the bell crank, means for loading the other arm of the bell crank to produce a tensional force in said cable, a cable-vibrating mechanism mounted upon one of said piers in engagement with said cable, said vibrating mechanism comprising an eccentrically-loaded ily wheel, and means for rotating said ily wheel at various speeds, said ily wheel being adjustable with respect to its eccentric loading.
  • a sleeve carried by the cable means at each end of the sleeve for rigidly securing it to the cable, antifriction bearings carrled by the sleeve adjacent to each and thereof, a frame having vertical guide members for engaging said bearings to coniine the sleeve to motion in a vertical plane, antifriction bearings on the sleeve at its mid-portion, a y wheel mounted concentrically with the sleeve and journailedA for rotation on the antifriction'bearings,
  • an eccentric loading ring carried by the fly wheel, means on the fly wheel for adjusting the position ofthe loading ring to move the center of gravity of the y wheel, and means for rotating the ily wheel to cause the cable to vibrate in the plane of the guide members at a frequency equal to the speed of rotation 'of the y wheel and with an amplitude proportional to the distance that the center of gravity of the fly wheel is displaced from its centers of rotation.
  • a fatigue testing machine comprising a'fly wheel mounted for rotation ⁇ and oscillation, a movable weight carried by the ily wheel for caus-l ing it to'oscillate, said weight being of annular shape and disposed adjacent the web of the fly wheel, set screws having conical inner ends for moving the weight radially within the y wheel, and a hub portion having a conical face for engaging the conical ends of the set screws so positioned that when the set screws are tightened the annular weight is forced into frictional engagement with the web of the ily wheel.

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  • Physics & Mathematics (AREA)
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  • Life Sciences & Earth Sciences (AREA)
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Description

March 27, 1934. R. TEMPLIN FATIGUE TESTING MACHINE Filed April 16. 1931 3 Sheets-Sheet HINVENTOR WM l?,
lll/111111.
March 27, 1934. R. L ,TEMPl-.IN
I FATIGUE TESTING MACHINE Filed April 16. 1951 5 Shee -Sh et 2 AINVENTOF? WITNESSES March 27, 1934. 'R L, TEMPLIN FATIGUE TESTING MACHINE 5 'sheets-shew?u 5 Filed April 16L 1951 WITNESSES Patented Mar. 27, 1934 PATENT OFFICE lFATIGUE TESTING MACHINE .Richard L. Templin, Parnassus, Pa., assigner to Aluminum Company vof America, Pittsburgh, Pa., a corporation of Pennsylvania `Application April 16, I1931, Serial No. 530,495
7 Claims.
This invention relates generally to the art of testing materials, and particularly to the testing of wires or cables to' determine their resistance to stresses set up by periodic forces.
In utilizing wires and cables in long spans as for instance in overhead lines for the transmission o f electrical energy, the cables are subjected, in addition to the tensile stresses set up in them ln supporting their own weight, to periodic stresses that result from vibrations. These undesirable vibrations are ordinarily set up by the wind or other forces causing the cable to oscillate in the direction transverse to its length. p It will be readily appreciated that it is diilicult to obtain data regarding the vibrations of cables when they are mounted in their operating positions for the reason that it is inconvenient to make the necessary measurements, and the oscillations cannot be controlled to provide data over a com- 20 plete range of conditions.
An `object of my invention is to provide apparatus for testing cables to determine their resistance to fatigue as the result of repeated stresses. A further object is to provide a cable- .25 testing apparatus capable of duplicating the conditionsl to which a cable is subjected when supported in a span of a transmission line'.,
In accordance with this invention, I provide supporting structures to which the ends of a cable to be testedare attached. The supporting structures are mounted, for instance on the floor of a building, in such manner that vibrations will not be transmitted from one structure to the other through the oor of-v the building, and suitable means are provided for applying predetermined tensile force to the cable. Suitable apparatus is provided, preferably mounted on one of the supporting structures, for causing the cable to vibrate in a. direction transverse to its length. This apparatus is mounted intermediate the ends of the cable to cause vibration in a longitudinal plane, and is adjustable to apply a predetermined force at predetermined frequency.
Particular apparatus for accomplishing this result and for achieving the stated and other obpects of the invention that will be apparent upon further consideration of this specification is described in detail herein and shown in the accompanying drawings, of which Fig. l is a more or less diagrammatic view in elevation of the cable-testing apparatus; Fig. 2 is a view in longitudinal section taken on the plane represented by the line II-H in Fig. 3, of the mechanism for causing the cable tor vibrate: Fig. 3 is a view, partlyA cable-vibrating mechanism taken on the plane represented by the line III-III of Fig. 2; Fig. 4 is a plan view, partly in horizontal section, of the cable-vibrating mechanism and its associated operating mechanism; and Fig. 5 is a view in cross section of the operating mechanism taken on the plane represented by the line V-V in Fig. 4.
Referring more particularly to the general view of the cable-testing mechanism in Fig. 1, the apparatus comprises two piers 1 and 2 for supporting, at its respective ends, a piece of wire or cable 3 to be tested. 'I'he supporting piers 1 and 2 are preferably massive bodies of concrete or of other. suitable material, supported on the oor 4 of a building by means of seals or pads 5 of non-resonant material, as for instance sand, to prevent extraneous vibrations from being transmitted from the oor 4 to the cable 3 by way of the piers, hence preventing transmission of vibrations through the floor from one end of the cable to the other. The piers may be spaced as desired to provide for receiving a piece of cable of suitable 4length for testing.
As shown, one end of cable 3 is rigidly secured to the pier 1 by means of any suitable anchor or cable clamp 6 attached at the rear edge of the pier 1 and elevated somewhat above its upper surface by means of a supporting structure 7 that may be made of I-beams or other structural elements. To enable predetermined tensile stresses to be set up in the cable 3, for duplicating the tensile stresses that occur in transmission-line cables, the other end of the cable is supported on pier 2 by means of an anchor 8 connected to one arm of a bell crank 9, pivoted on a bracket 1l at the back of the pier, on the other arm of which is suspended a weight 12. The eect of the weight 12 in applying tension to the cable may be changed .by adding to or taking from it disks 13, as is ordinarily done in adjusting the weights on a scale, or by providing any other convenient means for applying objects of known weight.
Mounted on pier 1 is a mechanism 20 for impressing upon the cable 3 periodic forces that set it to vibrating in such manner as to duplicate the vibrations of a cable constituting part of a transmission line. Such vibrations in a suspended cable may be caused by the wind, snow or ice loads, or by other forces'to which the transmission line may be subjected. As is well known, vibrations set up stresses within the material of the cable of a repeating nature that add to the initial tensile stress in the cable, and periodically raise the total stress to dangerously high values.
' It is also well known that, when subjected to repeated stresses of thisnature, material may fracture progressively and ultimately fail altogether from what is termed fatigue.
To enable a careful study to be made of the eiects of repeated stresses on a suspended cable, it is desirable that the conditions under which the test cable 3 -is caused to vibrate be readily predetermined and controlled. To accomplish -such control, the vibrating mechanism' 20 is designed to apply to the cable 3 transverse vibrations in one longitudinal plane o f the cable, of predetermined amplitude and frequency. This apparatus comprises essentially a ily wheel 21, jour-,
nalled to rotate around the cable 3 as a center. in a plane transverse to the cable. To effect vlbration of the cable 3, the fly wheel 21 is provided withan eccentrically mounted weight-22 which may be adjusted, relative to the center of rotation, to regulate the applied force and amplitude of vibration of the cable. To adjust the frequency of vibration, it is simply necessary to regulate the speed of rotation of the fly wheel.
As shown in detail in Fig. 2, the y wheel 21 is journalled for rotation by means of suitable ballbearings 23 on a substantially cylindrical sleeve or spindle that surroundsand is secured to the test cable 3. The ends of the sleeve 24 are disposed between pairs of vertical guides or standards 25 that constitute part of a frame 26 for the vibrating mechanism. The vertical guides 25V constrain the sleeveV 24, and consequently the cable 3, to motion in the vertical longitudinal plane of the cable.` For locking the sleeve 24 securely to the test cable 3, the sleeve is provided e -are in turn threaded on the exterior of the spindle 24. In accordance with well-known clamping action, as the retaining nuts 29 are turned onto the sleeves 24,`the fingers o r segments of collets 28 will be forced towards each other by the conical tores 27, and thus tightly grip the cables 3 in such manner that the spindle 24 becomes rigidly attached to it. To release the spindle 24 from thev cable 3 after a test has been completed, the
sleeves 31 may be unscrewed from the ends of the spindle, whereupon they engage the shoulders 30 and force the collets 28 out of conical bores 27.
Near each end, the sleeve 24 is providedwith encircling ball-.bearings 32 held in p1aceonl the sleeve by lock nuts 33, the outer races of said ball-bearings fitting between the guide plates or bearings 34 mounted on the guides V25 provided on the frame 26.
- To retain the sleeve 24 within the guides 25 and to strengthen the frame structure; the tops of the guides 25 in each pair are connected by a tie bar 35, near the middle of each of which there is an oil cup 36 from which oil is permitted to drip on the ball-bearings 32 to lubricate them and the guide plates 34. Such excess oil as may drip from the bearings is collected in the base of the frame 26. y
A `suitable chamber 37 is provided within the y wheel 21 for receiving lubricant, such as grease, for lubricating the ball-bearings .23 that support the fly wheel on the spindle 24. As best shown in Fig. 3, the eccentric weight 22 is in the shape of an annulus that encircles the hub of the fly wheel 21 and lies within a chamber 38 in one side of the wheel between the hub and the rim thereof. The eccentric loading ring 22 is supported in the chamber 38 by means of two set screws 39 which pass through diametrically opposed openings in the rim of the wheel 21 and are threaded in similarly aligned openings through the ring 22 in such manner that the screws 39 lie on a. diameter' of the wheel 21. As shown, the inner ends of the screws 39 contact with the hub of the wheel 21, and, in order to adjust the position o! the eccentric ring 22, it is merely necessary to loosen one of the screws and tighten the other screw to move the ring in the desired direction. 'To insure that the ring 22 will be held rmly in-lts adjusted position, the inner ends of the screws are made conical and bear at one side upon a4 conical surface 40 on the hub of the wheel 21 in such manner that when the screws are tightened they will tend to force the ring 22 sidewise into frictional engagement with the web of-the y wheel 21. In this manner the ring 22 will be prevented from moving relative to the fly wheel 21 while the vibrating mechanism is inv operation.
In order that the maximum range of adjustment may be had, the ring 22 is made with one side thicker than the other, as shown in Fig. 3, and so proportioned that when the thick or heavy side of the ring is adjacent to the hub of the wheel 21, as shown, the wheel 21 will be substantially in true running balance. As the ring 22 is moved from this position to its other extreme position, the degree of unbalance of the wheel is varied from zero to a maximum value. Hence by adjusting the position of the ring any desired degree of periodic force may be applied to the cable 3 within the limits of the apparatus.
The vibrating mechanism 20 is mounted on the pier 1 in such manner that it may be moved longitudinally thereof to position it relative to the xed end of the cable. As shown in Figs. 1 and 4, the frame 26 of the vibrating mechanism is secured to a base plate 41 that is in turn fastened on the upper surface of the pier 1 by anchor bolts 42. As shown in Fig. l, a plurality of bolts 42 are provided so spaced that the base plate 41 may be disposed in either one oi.` two positions on the pier at different distances from the end of the cable. This is accomplished by using three equally spaced pairs, or a total of six anchor bolts, and positioning the base plate to engage one pair of bolts. at each of its ends. Thus the base plate 41 may engage, at the appropriate end, one of the other end pair of bolts and at its other end, the
,f middle pair of bolts.
For accomplishing closer adjustment of the vibrating mechanism relative' to the end of the cable, the base plate 41 is provided with T-slots 43 extending longitudinally thereof and parallel to the cable 3. By means of bolts 44 having square heads disposed in rthe T-slots 43, the vibrating mechanism is mounted on the base plate 41 in such manner that it may be adjusted longitudinally to any position within the limits of the base plate. After being positioned it may be securely clamped in place by means of nuts 45 threaded on the Yupper ends of the bolts 44.
For rotating the y wheel 21 of the vibrating mechanism, 4a power transmission mechanism is supported adjacent thereto'on a suitable frame 47 that comprises two transverse angle elements 48 secured to the ends of 'the base plate 41 by means Qf nuts 49 threaded on the ends of the anchor bolts 42, 4in such manner that the frame overhangs the pier 1. The transmission mechanism comprises a suitable electric motor 51 con'- nected to drive the vibrating mechanism by means of a suitable speed changing device 52 that turns a cone pulley 53 from one Aface of which a belt 54 extends, in substantially horizontal direction, to a belt pulley 55 on the hub of the y wheel 21.
As shown in. Figs. 4 and 5, the variable speed mechanism 52 and the driving motor 51 are both mounted on a common bed plate 57 that is secured to a pair of longitudinal members 58 extending between the transverse members 48 of the frame 47. The entire bed plate 57, together with the motor 51 and the transmission mechanism 52, may be moved along the long'tudinal members 58 of the frame 47 to bring any one of the three faces of the cone pulley 53 into alignment with the belt pulley 55 on the fly wheel of the vibrating mechanism.
After the belt pulleys have been thus aligned and the belt 54 placed in position, the belt may be tightened by moving the entire driving mechanism'and its bed plate 57 in the direction away from the vibrating mechanism. This is accomvplished by means of a well known adjusting screw 61 that is journalled in the bed plate 57 and has screw threaded engagement with an adjusting block 62 carried by a clamping plate 63 tted between the longitudinal members 58. As shown, the adjusting block 62 is disposed adjacent one of the longitudinal members 58, and there is provided adjacent the other longitudinal member a similarly shaped clamp'ng block 64. The blocks 62 and 64 are each provided with downwardly extending threaded shanks passing through the clamping plate 63 Aand provided at their lower ends with clamping nuts 65. After the bed plate 57 has been adjusted to align the belt pulleys, and the belt has been tightened by turning the adjusting screw 61, the entire transmission mechanism may be securely clamped to the frame- 4 7 by tightening the clamping nuts 65 on the adjusting block 62 and the clamping block 64 to draw the clamping plate 63 into firm engagement with the longitudinal members 58, and to prevent further rotation of the adjusting screwV 61.
The variable speed-transmission mechanism 52 is of the friction type, comprising a frame 71 in which a shaft 72 is journalled on antiefriction bearings 73 at right angles to the shaft of the motor 51. The cone pulley 53 is mounted on one end of the shaft, and at the other end is mounted a friction wheel 74 driven in a well known manner by a friction disk 75 carried on the shaft of the driving motor 51. To urge the disk 75 into contact with the wheel 74, the motor shaft is provided, at its other end, with an adjustable thrustV bearing mechanism 76. To adjust the speed at which the fly wheel 21 is operated, it is merely necessary to move the driving motor 51 relative to the friction wheel 74 to cause the wheel 74 to bear on the friction disk.75 at a. position having a different radius of rotation. This adjustment is accomplished by moving the motor 51 in guideways 78 on the base plate 57 in such manner that it may be moved parallel to the shaft 72 on which the friction wheel 74 is mounted.' The motor may be adjusted to the de'sn'ed position along the guideways 78 by means of a screw-thread adjusting mechanism 79 that may be operated by means of a hexagonal fitting 80 at the end of the shaft.
In performing a testing operation, a sample of the cable to be tested is passed through the sleeve 24 of the vibrating mechanism 20 and suspended between the piers 1 and 2 in the manner described. Initial tension is applied to the cable 3 by attaching the required amount of weights 13 to the bell-crank 9, and theA eccentric weight 22 is adjusted to exert the desired amount of force to vibrate the cable. The frequency at which the force is to be applied is thenregulated by adjust-1,` ing the variable speed mechanism 52. The appa-v ratus may then be operated until the cable 3 breaks from fatigue failure, or if the cable does not fail, the test may be continued for a predetermined number of reversals of stress in the cable. The total number of reversals of stress imposed upon the cable 3 during a test may be recorded by means of a revolution counter 81 mounted on the transmission mechanism 52 and actuated by the shaft 72.
Although I have shown and described only one specific embodiment of my invention, it is self evident that the apparatus for practicing the invention may be constructed in many other ways, and it is to be understood that the specific terms used in describing the various partsof the apparatus are for the purpose only of clearly disclosing a workable embodiment of the invention and are not to be interpreted as limiting the spirit and scope of the invention as defined in the appended claims.
I claim:
l. A cable testing apparatus comprising spaced supporting structures for supporting at its ends a cable to be tested, said supporting structures including non-resonant bases to isolate the same from each other and their surroundings, means for applying a tensional force to said cable, and means for imparting vibrations to the cable in a direction transverse to its length, said vibration-imparting means comprising an eccentrically-loaded iiy wheel mounted for rotation upon and positioned intermediate the ends of said cable.
2. A cable testing apparatus comprising a pair vof isolated supports, means for suspending a cable lmounted for longitudinal movement with respect to the ends of said cable.
3. A cable testing apparatus comprising spaced supporting structures for supporting at itsends a cable to be tested, a sleeve mounted on said cable in spaced relation to one end thereof, vertical guides disposed at each side of said sleeve, a fly wheel having an adjustable eccentric weight rotatably mounted on said sleeve and means for rotating theeccentrically-weighted -fly wheel whereby the cableis vibrated in a vertical longitudinal plane.
4. In a cable testing mechanism, a cable-vibrating device adapted to be positioned intermediate the ends of a suspended cable, said device comprising a sleeve secured to said cable, a fly wheel rotatably mounted on said sleeve, and means for driving said ily wheel, said driving means comprising a motor-driven adjustable speed transmission whereby the frequency of vibration may be varied.
'5. A cable testing apparatus comprising means for suspending a cable to be tested, vsaid means comprising massive supporting piers arranged in spaced relationship upon non-resonant bases, a cable clamp mounted on one of said piers, a bell crank pivotally mounted on said other pier, said cable having one end' attached to the cable clamp and its opposite end attached to one arm of the bell crank, means for loading the other arm of the bell crank to produce a tensional force in said cable, a cable-vibrating mechanism mounted upon one of said piers in engagement with said cable, said vibrating mechanism comprising an eccentrically-loaded ily wheel, and means for rotating said ily wheel at various speeds, said ily wheel being adjustable with respect to its eccentric loading.
6. In apparatus'for testing a cable supported at its ends, in combination, a sleeve carried by the cable, means at each end of the sleeve for rigidly securing it to the cable, antifriction bearings carrled by the sleeve adjacent to each and thereof, a frame having vertical guide members for engaging said bearings to coniine the sleeve to motion in a vertical plane, antifriction bearings on the sleeve at its mid-portion, a y wheel mounted concentrically with the sleeve and journailedA for rotation on the antifriction'bearings,
an eccentric loading ring carried by the fly wheel, means on the fly wheel for adjusting the position ofthe loading ring to move the center of gravity of the y wheel, and means for rotating the ily wheel to cause the cable to vibrate in the plane of the guide members at a frequency equal to the speed of rotation 'of the y wheel and with an amplitude proportional to the distance that the center of gravity of the fly wheel is displaced from its centers of rotation.
7z A fatigue testing machine, comprising a'fly wheel mounted for rotation`and oscillation, a movable weight carried by the ily wheel for caus-l ing it to'oscillate, said weight being of annular shape and disposed adjacent the web of the fly wheel, set screws having conical inner ends for moving the weight radially within the y wheel, and a hub portion having a conical face for engaging the conical ends of the set screws so positioned that when the set screws are tightened the annular weight is forced into frictional engagement with the web of the ily wheel.
` RICHARD L. TEMPLIN.
US530495A 1931-04-16 1931-04-16 Fatigue testing machine Expired - Lifetime US1952953A (en)

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2469346A (en) * 1945-06-14 1949-05-03 Budd Co Fatigue-testing machine
US3110174A (en) * 1961-09-05 1963-11-12 Int Harvester Co Test device for earth working tool
US3344995A (en) * 1964-07-15 1967-10-03 Ronald A Koetters Method and apparatus for disintegrating concrete and like materials
US9372137B1 (en) 2013-08-20 2016-06-21 Google Inc. Tension member fatigue tester using transverse resonance

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2469346A (en) * 1945-06-14 1949-05-03 Budd Co Fatigue-testing machine
US3110174A (en) * 1961-09-05 1963-11-12 Int Harvester Co Test device for earth working tool
US3344995A (en) * 1964-07-15 1967-10-03 Ronald A Koetters Method and apparatus for disintegrating concrete and like materials
US9372137B1 (en) 2013-08-20 2016-06-21 Google Inc. Tension member fatigue tester using transverse resonance
US9557255B2 (en) 2013-08-20 2017-01-31 X Development Llc Tension member fatigue tester using transverse resonance

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